View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 17234.56689416 -.00000007 +00000-0 +27711-4 0 9990
2 24278 098.5532 108.9656 0350620 165.2425 195.9272 13.53077752037604
| Epoch (UTC): | 22 August 2017 13:36:19 |
| Eccentricity: | 0.0350620 |
| inclination: | 98.5532° |
| perigee height: | 800 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 108.9656° |
| argument of perigee: | 165.2425° |
| revolutions per day: | 13.53077752 |
| mean anomaly at epoch: | 195.9272° |
| orbit number at epoch: | 3760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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